An atomization and drop breakup model for high-pressure-driven liquid fuel sprays is presented, tuned, and validated. The breakup criterion is determined by the Taylor drop oscillator, and each breakup event reflects the experimentally observed drop disintegration mechanism of either bag, stripping, or catastrophic breakup. The formation of a fragmented liquid core resulting from inner-nozzle disturbances is achieved by subjecting the initial drops to a primary breakup process followed by a cascade of drop breakups. The primary breakup is simulated by providing the injected drops with appropriate initial deformation velocities such that experimentally observed breakup lengths are obtained. The model has been timed and validated by means of ...
Flash-boiling of fuel sprays can occur under injection of superheated fuel into ambient pressure tha...
The overall performance of direct injection (DI) engines is strictly correlated to the fuel liquid s...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77144/1/AIAA-23475-448.pd
A further development of the ETAB atomization and drop breakup model for high pressure-driven liquid...
In this paper a breakup model for analysing the evolution of transient fuel sprays characterised by ...
AbstractIn this paper a breakup model for analysing the evolution of transient fuel sprays character...
A model is currently under development to predict the occurrence and outcome of spray droplet breaku...
Liquid droplet breakup and dynamics is a phenomena of immense practical importance in a wide variety...
This paper presents numerical simulations of the atomization of viscous liquids, focusing on the com...
The present paper addresses the macroscopic atomization characteristics of liquid-fuel droplets when...
A unified approach towards modeling fuel sprays for internal combustion engines has been developed i...
A theoretical and experimental study of the dense-spray region of pressure-atomized nonevaporating s...
The dispersed-phase structure of the dense-spray region of pressure-atomized sprays was studied for ...
In this paper we examine droplet behavior and macroscopic atomization characteristics of a non-react...
Sprays are used in a wide range of engineering applications, in the food and pharmaceutical industry...
Flash-boiling of fuel sprays can occur under injection of superheated fuel into ambient pressure tha...
The overall performance of direct injection (DI) engines is strictly correlated to the fuel liquid s...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77144/1/AIAA-23475-448.pd
A further development of the ETAB atomization and drop breakup model for high pressure-driven liquid...
In this paper a breakup model for analysing the evolution of transient fuel sprays characterised by ...
AbstractIn this paper a breakup model for analysing the evolution of transient fuel sprays character...
A model is currently under development to predict the occurrence and outcome of spray droplet breaku...
Liquid droplet breakup and dynamics is a phenomena of immense practical importance in a wide variety...
This paper presents numerical simulations of the atomization of viscous liquids, focusing on the com...
The present paper addresses the macroscopic atomization characteristics of liquid-fuel droplets when...
A unified approach towards modeling fuel sprays for internal combustion engines has been developed i...
A theoretical and experimental study of the dense-spray region of pressure-atomized nonevaporating s...
The dispersed-phase structure of the dense-spray region of pressure-atomized sprays was studied for ...
In this paper we examine droplet behavior and macroscopic atomization characteristics of a non-react...
Sprays are used in a wide range of engineering applications, in the food and pharmaceutical industry...
Flash-boiling of fuel sprays can occur under injection of superheated fuel into ambient pressure tha...
The overall performance of direct injection (DI) engines is strictly correlated to the fuel liquid s...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77144/1/AIAA-23475-448.pd